Method for processing flight data

Patent metadata

Field	Value
Publication number	US-12339653-B2
Application number	US-202117914164-A
Country	US
Kind code	B2
Filing date	Mar 23, 2021
Priority date	Mar 26, 2020
Publication date	Jun 24, 2025
Grant date	Jun 24, 2025

Abstract

A method for processing flight data having been recorded during three or more flights of an aircraft by a flight data recorder including obtaining two signature vectors with respective sizes, the two signature vectors corresponding to two different flights among the three or more flights, determining a similarity matrix, the components of which quantify the proximity between the two flight signature vectors, each component allowing identifying, for each element of a first signature, an element of the other signature which is closest, the proximity between two components of the signature vectors being a distance weighted by a mean value of the neighboring components of the similarity matrix, repeating the obtaining and determining in order to compare, two by two, all the flight signatures so as to obtain three or more similarity matrices, and processing said similarity matrices in order to evaluate the similarity between two flights.

First claim

The invention claimed is:

1. A computer implemented method for processing flight data, the computer implemented method comprising:
E 1 ) receiving from a flight data recorder of an aircraft, flight data recorded during at least three flights of at least one aircraft by means of the flight data recorder, the data being grouped by flight in a signature vector of the flight, the components of which correspond to data recorded during said flight of the aircraft, a flight being defined by a signature vector,
E 2 ) obtaining two signature vectors x and y with respective size l and m, l≤m, the two signature vectors corresponding to two different flights among said at least three flights;
E 3 ) determining a similarity matrix D the components D (i,j) of which quantify the proximity between the two flight signature vectors x and y, each component allowing identifying for each element of the signature x an element of the other signature y which is closest, the proximity between two components of the signature vectors x and y being a distance weighted by a mean value of the neighboring components of the similarity matrix,
wherein determining the similarity matrix comprises:
E 31 ) initializing a matrix D having L rows and C columns, L=l+1 and C=m−l+2 columns;
E 32 ) calculating D(1,1)=|x 1 −y 1 | 2 and for (i,j)(i,j)≠(1,1);
E 33 ) calculating the elements D[i,j]=|x i −y i+j−1 | 2 +A+B;
with

A
=

i
-
1

(

i
+
j
-
2

)

×

D
[

i
-
1

,
j

]

;
and

B
=

j
-
1

(

i
+
j
-
2

)

×

D
[

i
,

j
-
1

]

;

i
=
1

,
…

,

l
⁢

and
⁢

j

=
1

,
…

,

m
-
l
+
1

;

E 4 ) repeating steps E 2 ) and E 3 ) in order to compare, two by two, all the flight signatures so as to obtain at least three similarity matrices; and
E 5 ) processing said similarity matrices D in order to evaluate the similarity between two flights.

2. The method according claim 1 , wherein the processing E 5 ) comprises the following sub-steps:
E 51 ) decomposing into eigenvectors and eigenvalues each similarity matrix D;
E 52 ) determining an entropy coefficient for each eigenvalue;
E 53 ) selecting a subset of eigenvectors such that the sum of the entropies is greater than a fraction of the sum of the entropies;
E 54 ) determining for each signature, based on the selected eigenvectors, an abnormality score for the purpose of evaluating whether a flight is abnormal.

3. The method according to claim 2 , wherein for each abnormal flight detected, a ghost flight is determined that is closest to the abnormal flight detected which having an abnormality score such that the flight is normal.

4. The method according to claim 3 , wherein the parameters of the abnormal flight detected are compared to those of the ghost flight determined in order to detect at least one parameter of the abnormal flight which caused said detected abnormal flight to be abnormal.

5. The method according to claim 4 , further comprising displaying the abnormal flight.

6. A non-transitory computer program product comprising code instructions which, when executed by a processor, cause the processor to perform the method according to claim 1 .

7. A system for processing flight data comprising:
a flight data recorder of an aircraft located on an aircraft, the flight data recorder being configured for acquiring flight data during a flight of an aircraft; and
a ground station in communication with the flight data recorder, the ground station comprising a processor that implements the method as claimed in claim 1 .

Assignees

• Safran Electronics & Defense
• Univ De Technologie De Troyes
• Univ De Technologie De Compiegne

Inventors

• Chrysanthos Nicolas
• Ferrand Fabrice
• Beauseroy Pierre Jean Emile

Classifications

• G07C5/0808

  Diagnosing performance data (testing of vehicles G01M17/00; testing of electrical installation on vehicles G01R31/005) · CPC title

• G07C5/008

  communicating information to a remotely located station (transmission systems for measured values G08C) · CPC title

• G06F18/22

  Matching criteria, e.g. proximity measures · CPC title

• G06F2218/16

  by matching signal segments · CPC title

• G05B23/0237 Primary

  based on parallel systems, e.g. comparing signals produced at the same time by same type systems and detect faulty ones by noticing differences among their responses · CPC title